Adjustable shovel element of a gas turbine of an aircraft engine, comprises adjusting device for changing shape of adjustable shovel element, which is constructed by a generative manufacturing process

摘要

Adjustable shovel element (1), preferably an adjustable shovel element of a gas turbine of an aircraft engine, comprises at least one adjusting device (17) for changing the shape of the adjustable shovel element. The adjustable shovel element together with the adjusting device is constructed by a generative manufacturing process. An independent claim is also included for constructing the adjustable shovel element, preferably the adjustable shovel element of the gas turbine of the aircraft engine, comprising constructing the adjustable shovel element having the adjusting device by the generative manufacturing process.